Research Article
A New Adaptive Federated Cubature Kalman Filter Based on Chi-Square Test for SINS/GNSS/SRS/CNS Integration
Table 1
Parameters in simulations.
| | Initial position | East longitude | 108.9° | | North latitude | 34.025° | | Altitude | 40 km |
| | Initial velocity | East | 151 m/s | | North | 125 m/s | | Up | 125 m/s |
| | Initial attitude | Pitch | 0° | | Roll | 0° | | Yaw | 0° |
| | Gyro parameters | Constant drift | 0.5°/h | | White noise | 0.5°/h | | Sampling frequency | 10 Hz |
| | Accelerometer parameters | Zero bias | 0.1 mg | | White noise | 0.1 mg | | Sampling frequency | 10 Hz |
| | GNSS parameters | Pseudorange measurement error | 20 m | | Pseudorange rate measurement error | 0.5 m/s | | Sampling frequency | 10 Hz |
| | SRS parameters | Redshift measurement error | 10^-8 | | Sampling frequency | 1Hz |
| | CNS parameters | Measurement error | 15m | | Sampling frequency | 1Hz |
| | Barometric altimeter parameter | Altitude measurement error | 10m | | Sampling frequency | 1Hz |
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